Flap Cross Shaft Assembly - Jabiru j160 Technical Manual

Aircraft Technical Manual
JTM001-5
Figure 113 – J200 Family Electric Flap System Sheet 2 (J200/J400, J230/J430, J250/J450)
6.58 FLAP Cross SHAFT ASSEMBLY (all J-Series)
6.58.1 Description

As shown above the flaps are driven via a shaft which runs from one side of the fuselage to the
other.

In turn this shaft is an assembly of 2 different sized steel tubes with input and output arms attached.
6.58.2 Flap Cross Shaft Removal
Required Tools:
Parts and Material:
Type of Maintenance:
Level of Certification:
Return to Service:
1. Remove one wing to allow removal of shaft. Refer to Section 0 for details on wing removal
procedure.
2. Either use heavy duty tape to hold the remaining flap in the up position or remove the flap
from the aircraft.
3. Disconnect the flap drive motor or manual lever from the cross shaft input arm.
4. Remove external flap drive arm from the end of the shaft nearest the remaining wing.
This document is controlled while it remains on the Jabiru server. Once this no longer applies the document becomes uncontrolled.
ISSUE 1 2 3
Jabiru Aircraft
J120, J160, J170, J200/J400, J230/J430, J250/J450 Variants
Tools as required in Section 0
Heavy duty tape
Line Maintenance
L2 or LAME (A&P or LSA Repairman / Maintenance)
L2 or LAME (A&P or LSA Repairman / Maintenance)
4 5 Dated: 29th October 2014
Pty Ltd
Issued By: AS Page: 163 of 298